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Aircraft Engine Historical Society, Inc.

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Found in 814 Collections and/or Records:

"Interference Effects of Single and Multiple Round or Slotted Jets on a VTOL Model in Transition" (NASA Technical Note TN D-2380), 1964-08

 Item — Box MC-019-002, Folder: 001.A.056
Identifier: 20060043
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-2380, dated August 1964.

Scope: Preliminary NASA research report by Raymond D. Vogler of Langley Research Center, Langley Station, Hampton, Va.

Contents: See title.

Dates: Publication: 1964-08
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

"Interior Corrosion of Steel Struts and its Prevention" (Air Service Information Circular (Aviation) Vol. IV, No. 374), 1922-06-05, 1922-09-01

 Item — Box MC-019-001, Folder: 001.A.014
Identifier: 20141379
Scope and Contents

Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Air Service Information Circular (Aviation) Vol. IV, No. 374 (September 1, 1922), based on McCook Field Report Serial No. 1949 (dated June 5, 1922).

Scope: Material Section Report No. 172, prepared by V. M. Wade, Material Section, Engineering Division, Air Service, McCook Field.

Contents: See title.

Dates: 1922-06-05; Publication: 1922-09-01
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

"Intermittent Oil Feed Investigations" (Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A, Vol. II, No. 3) [Photocopy], 1918-12

 Item — Box MC-019-001, Folder: 001.A.007
Identifier: 20140707
Scope and Contents Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A. [United States Army], Vol. II, No. 3 (dated December 1918). This section on pages 122 through 142.Scope: By the Experimental Department. Intended for limited, controlled distribution (see General note on publication data).Contents: article includes "Relations between Quantity,...
Dates: Publication: 1918-12
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.B: Aircraft Engine (Motor) RDT&E

"Internal Bracing of Airplane Wings and Fuselage" (Bureau of Aeronautics Technical Note No. 34) [Photocopy], 1923

 Item — Box MC-019-001, Folder: 001.A.021
Identifier: 20152034
Scope and Contents

Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Navy Department, Bureau of Aeronautics Technical Note No. 34 (dated 1923), based on "Reprint of Navy Department, Bureau of Construction and Repair A. T. N. [Aeronautical Technical Note] No. 88)".

Scope: Report #40584-23 is "From A British Source".

Contents: See Title.

Dates: Publication: 1923
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

"Internal Stresses in Liberty 12-A" (Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A, Vol. II, No. 1), 1918-10

 Item — Box MC-019-001, Folder: 001.A.005
Identifier: 20140705
Scope and Contents Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A. [United States Army], Vol. II, No. 1 (dated October 1918). This section on pages 66 through 82.Scope: By Final Design Section. Intended for limited, controlled distribution (see General note on publication data).Contents: article includes "Analysis of Gas and Dynamic Loadings...
Dates: Publication: 1918-10
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.B: Aircraft Engine (Motor) RDT&E

Introduction to Aerodynamics of a Compressible Fluid, 1947, 1947

 Item — Special collection MC-19, Book: 047, Call No.: TL 574 .C4 L5
Identifier: 20061121
Scope and Contents Document Type: Book (Technical)Purpose: Authoritative Reference.Authority: Author Expertise.Series: Galcit Aeronautical SeriesScope (from Author's Preface): "The subject, Aerodynamics of Compressible Fluids, has been studied at great length by both pure mathematicians and "practical" engineers, and the literature on the subject has become extensive. The material presented in this book is designed to furnish the reader...
Dates: Copyright: 1947; Publication: 1947
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.E: Aeronautical RDT&E (Special Collection)

Introduction to Aircraft Design, 1942, 1942

 Item — Special collection MC-19, Book: 058, Call No.: TL 671.2 .F384
Identifier: 20061177
Scope and Contents Document Type: Textbook (Technical).Purpose: Training and Education.Authority: Author Expertise.Scope (from Preface): "The purpose of this book is to bridge the gap between the field of aeronautical engineering and airplane design and the other professional fields of engineering, architecture, and general design. The material originated in a course conducted by the University of California as part of its Engineering, Science, and...
Dates: Copyright: 1942; Publication: 1942
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series II: Aircraft (commercial & military) / Sub-series II.E: Aircraft (Special Collection)

"Inverted Liberty Zenith Carburetors" (Bulletin of the Experimental Department, Airplane Engineering Division, U.S.A, Vol. II, No. 4) [Photocopy], 1919-01

 Item — Box MC-019-001, Folder: 001.A.008
Identifier: 20140708
Scope and Contents Document Type: Technical Research Report Authority: Government Military (authoritative reference) Document Number: Bulletin of the Airplane Engineering Department, U.S.A. [United States Army], Vol. II, No. 4 (dated January 1919). This section on pages 107 through 118 and 139.Scope: By the Experimental Department. Intended for limited, controlled distribution (see General note on publication data).Contents: article includes "New Arrangement for Mounting Above Intake...
Dates: Publication: 1919-01
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.B: Aircraft Engine (Motor) RDT&E

"Investigation in the Langley 19-Foot Pressure Tunnel of Two Wings of NACA 65-210 and 64-210 Airfoil Sections with Various Type Flaps" (NACA Report No. 942), 1949

 Item — Box MC-019-001, Folder: 001.A.026
Identifier: 20060147
Scope and Contents

Document Type: Technical Research Report. Authority: Government Civil (authoritative reference). Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 942, published in 1949.

Scope: NACA research report by James C. Sivells and Stanley H. Spooner.

Contents: See title.

Dates: Publication: 1949
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

"Investigation of A Semispan Tilting-Propeller Configuration and Effects of Ratio of Wing Cord to Propeller Diameter on Several Small-Cord Tilting-Wing Configurations at Transitions Speeds" (NASA Technical Note TN D-1815), 1963-07

 Item — Box MC-019-002, Folder: 001.A.051
Identifier: 20060026
Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NASA Technical Note TN D-1815, dated July 1963.

Scope: Preliminary NASA research report by Kenneth P. Spreemann of Langley Research Center, Langley Station, Hampton, Va.

Contents: See title.

Dates: Publication: 1963-07
Found in: The University of Alabama in Huntsville Archives & Special Collections / Aircraft Engine Historical Society Collection / Series I: Aeronautical Research, Development, Test & Evaluation (RDT & E) / Sub-series I.A: Aircraft RDT&E

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